Page 113 - Entrophy Analysis in Thermal Engineering Systems
P. 113

106                              Entropy Analysis in Thermal Engineering Systems



          where Λ is a stochiometric coefficient. The number of moles of air supplied
          to combust one mole of fuel is 4.76Λ. The minimum value of Λ corresponds
          to stoichiometric combustion: Λ min ¼ x +   . Also, n v denotes the num-
                                               y
                                                  z
                                               4  2
          ber of moles of water vapor in the gaseous products, which depends on its
          partial pressure [1].
                                            ð
                                         p sat T 0 Þ
                                     n v
                                       ¼                               (8.7)
                                            p 0
                                     n p
          where p sat (T 0 ) is the saturation pressure of water at ambient temperature, and
          n p is the total number of moles of combustion products in the gas phase.

                                        y
                                n p ¼ n v   +  z  +4:76Λ               (8.8)
                                        4   2
          The combustion of one mole of fuel with 4.76Λ moles of air yields n p moles

          of gaseous products and  y   n v moles of liquid water. The molar enthalpies
                                2
          and entropies of the air, fuel, and combustion products are determined per
          unit mole of the fuel.
              1
                       f    p                              y
                  a              ð              Þ + h f ,0
                                                 a
                       0
                  0
                 H + H  H   0  ¼ Λh O 2  +3:76Λh N 2 0       n v h H 2 O l ðÞ,0
                                                           2
              _ n f
                        h                                             i
                                                                       p
                                                      z
                                                  y
                                        + Λ x  +
                        xh CO 2  + n v h H 2 O vðÞ      h O 2  +3:76Λh N 2
                                                  4   2                0
                                                                       (8.9)
          Recalling that both the air and fuel are supplied to the system at ambient
          conditions, Eq. (8.9) can be simplified to
            1                  h                        i
                     f    p                    y                y  z
                a            ¼ h f ,0  xh CO 2 ,0        + x +
                     0
                0
               H + H  H   0                      h H 2 O lðÞ,0        h O 2 ,0
                                               2                4  2
            _ n f
                                   h                i
                                            h H 2 O lðÞ ,0
                                 n v h H 2 O vðÞ,0
                                                                      (8.10)
          Taking the reference temperature and pressure T 0 ¼ 298.15 K and p 0 ¼ 1
          bar, the first three terms on the right-hand-side of Eq. (8.10) constitute the
          higher heating value (HHV) of the fuel, and the fourth term is zero because
          h O 2 ,0 ¼0. The enthalpy difference in the last term is the enthalpy of evap-
          oration of water, L . Hence, Eq. (8.10) reduces to
                           w
                           0
   108   109   110   111   112   113   114   115   116   117   118